A recoverable rocket and an associated recovery method are disclosed. A recoverable rocket comprises a rocket body and at least two side wings. One end of each side wing is connected to the casing of the rocket body, and the other end is connected to a deceleration mechanism; the deceleration mechanism comprises a turbine engine and a propeller. The propeller is arranged below the turbine engine. The propeller is connected to the drive shaft of the turbine engine, and the turbine engine drives the propeller to rotate in the air to generate a thrust which decelerates the rocket during recovery. The rocket body comprises a structural system, a propulsion system, a control system and a set of landing legs. The advantage of this invention is that it realizes the recovery of rockets.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Recoverable Rocket and an Associated Recovery Method


    Beteiligte:
    JIANG JIANTANG (Autor:in)

    Erscheinungsdatum :

    27.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Recoverable rocket and an associated recovery method

    JIANG JIANTANG | Europäisches Patentamt | 2025

    Freier Zugriff

    Recoverable rocket and recovery deceleration method thereof

    JIANG JIANTANG | Europäisches Patentamt | 2023

    Freier Zugriff

    Recoverable Rocket Vehicle

    H. F. Wuenscher | NTIS | 1965


    Recoverable Nuclear Rocket Freighter

    A. H. Flagg / H. S. McQueen / L. E. White | NTIS | 1959


    Recoverable rocket vehicle Patent

    Wuenscher, H. F. | NTRS | 1965